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Volume 38 Issue 8
Aug.  2012
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Journal of Beijing University of Aeronautics and Astronautics  > 2012  >  38(8): 1124-1128.
Hou Yunyi, Jing Qianfeng, Ma Guangfuet al. Orbital rendezvous control method for berthing and tracking approach[J]. Journal of Beijing University of Aeronautics and Astronautics, 2012, 38(8): 1124-1128. (in Chinese)
Citation: Hou Yunyi, Jing Qianfeng, Ma Guangfuet al. Orbital rendezvous control method for berthing and tracking approach[J]. Journal of Beijing University of Aeronautics and Astronautics, 2012, 38(8): 1124-1128. (in Chinese)
shu

Orbital rendezvous control method for berthing and tracking approach

  • 1.

    School of Astronautics, Harbin Institute of Technology, Harbin 150001, China

  • 2. Shanghai Aerospace System Engineering Institute, Shanghai 201108, China

  • Received Date: 06 Jan 2011
  • Publish Date: 30 Aug 2012
    Abstract
  • The spacecraft orbital rendezvous technology is required for many missions, and the requirements of orbital control vary with the different tasks. In some cases, the tracker will be asked to stop in specified position temporarily; in other cases, the line-of-sight angle and trajectory are limited in the process of orbital rendezvous. To meet the different needs of various tasks, a closed-loop feedback control law was designed. By using this method of orbital control, the tracker can stop and keep in fixed point and approach target along the predetermined trajectory. The simulation shows that the control method has the advantages of fast tracking speed, high-accuracy, and low power consumption.

     

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    • References(6)
  • [1]
    林来兴.空间交会对接技术[M].北京:国防工业出版社,1995 Lin Laixing.Space rendezvous and docking technology[M].Beijing: National Defence Industry Press,1995(in Chinese)
    [2]
    王颖,吴宏鑫,解永春.基于视线制导的交会停靠控制方法[J].航天控制,2004,22(6):21-24 Wang Ying, Wu Hongxin,Xie Yongchun.Line of sight guidance based rendezvous and berthing control method [J].Areospace Control, 2004,22(6):21-24(in Chinese)
    [3]
    朱仁璋,尹艳.论空间交会最终平移段制导设计[J].中国空间科学技术,2004,5:1-8 Zhu Renzhang, Yin Yan.Guidance strategy design for the final translation of space rendezvous [J].Chinese Space Science and Technology,2004,5:1-8(in Chinese)
    [4]
    Hablani H B.Guidance and relative navigation for autonomous rendezvous in a circular orbit[J].Journal of Guidance, Control and Dynamics, 2002,25(3):553-562
    [5]
    陈统.空间自主交会的轨道动力学与控制方法研究 .北京:北京航空航天大学,宇航学院,2008 Chen Tong, A study on orbital dynamics and control of space autonomous rendezvous .Beijing:School of Austronautics,Beijing University of Aeronautics and Astronautics,2008(in Chinese)
    [6]
    Singla P,Subbarao K,Junkins J L.Adaptive output feedback control for spacecraft rendezvous and docking under measurement uncertainty[J].Journal of Guidance, Control, and Dynamic, 2006, 29(4):892-902
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